# N336EN: 1992 Dehavilland DHC-8-311, registration cancelled 2020-03-20

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 20, 2020
- Exported to: Kenya
- Status when cancelled: Valid registration
- Airframe: [Dehavilland DHC-8-311](https://openairdocs.org/model/dehavilland-dhc-8-311) (registry code 2809005)
- Engine: [Pratt & Whitney Canada PW123](https://openairdocs.org/engine/pratt-whitney-canada-pw123) (registry code 52129)
- Data sheets: [TCDS A13NM](https://openairdocs.org/tcds/A13NM), [TCDS E20NE](https://openairdocs.org/tcds/E20NE) (OpenAirDocs)
- Serial number: 336
- Year built: 1992
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, transport
- Airworthiness date: September 29, 2000
- Certificate issued: January 10, 2007
- Last registry action: February 22, 2019
- Mode S code: A3AC8A
- Owner when cancelled: [Wells Fargo Trust Co Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20TRUST%20CO%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N336EN
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=336EN
- Page: https://openairdocs.org/deregistered/N336EN-2020-03-20

From the FAA registry file of November 3, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Dehavilland DHC-8-311: https://openairdocs.org/model/dehavilland-dhc-8-311.md

## Service difficulty reports (152, newest 50)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR A8ZR20200207001](https://openairdocs.org/sdr/A8ZR20200207001), Jan 14, 2020: SKIN. ERODED. AFT CARGO DOOR SKINAT FS 639 TO HAVE EROSION DAMAGE IN 2 LOCATIONS. AFTER DAMAGE REMOVAL THE FWD DAMAGE MEASURES .8"L X .140"W, AND THE AFT DAMAGE MEASURES 2.1"
- [SDR HNAA2018042700088](https://openairdocs.org/sdr/HNAA2018042700088), Apr 25, 2018: PROXIMITY SENSOR. OUT OF ADJUST. SERVICE DOOR OPEN INDICATION ILLUMINATED SHORTLY AFTER TAKEOFF ROLL WAS INITIATED. ADJUSTED AND TESTED THE SERVICE DOOR PROXIMITY SENSOR IAW MM 52-70-00, OPS CH
- [SDR HNAA2018032600068](https://openairdocs.org/sdr/HNAA2018032600068), Mar 23, 2018: STALL WARNING. FALSE ACTIVATION. NR 2 STALL SYSTEM FAIL AND PUSHER SYSTEM FAILED. CAUTION LIGHTS ILLUMINATED ON TAKEOFF ROLL. CYCLED SWSP COMP CIRCUIT BREAKERS, STALL SYSTEM 1 AND 2 TESTED NORM
- [SDR HNAA2017110700369](https://openairdocs.org/sdr/HNAA2017110700369), Nov 6, 2017: CONTROLLER. FAILED. AFCS CONTROLLER INOPERATIVE MESSAGE ON 802 PANEL. R & R AFCS CONTROLLER IAW AMM 22-10-01. OPS CHECKED BAD.
- [SDR HNAA2017101000345](https://openairdocs.org/sdr/HNAA2017101000345), Oct 6, 2017: PROPELLER. VIBRATION. MODERATE VIBRATION FROM THE RT PROPELLER. CONSTANT AND WORSENS WITH PROPELLER SPEED CHANGES. R & R THE NR 200 PROPELLER ASSY IAW CARD 61-10-06R, RAN ACFT IAW MO
- [SDR HNAA2017092500329](https://openairdocs.org/sdr/HNAA2017092500329), Sep 20, 2017: CONTROL UNIT. MALFUNCTIONED. REJECTED TAKE OFF. AUTOFEATHER FAILED TO ARM DURING TAKEOFF. TORQUE WAS AT 88%. R & R THE NR 2 TSCU IAW IAW MM 72-01-10. RAN AIRCRAFT, OPS CHECKED GOOD IAW PDT-
- [SDR HNAA20170918314](https://openairdocs.org/sdr/HNAA20170918314), Sep 15, 2017: CIRCUIT BREAKER. MALFUNCTIONED. REJECTED TAKEOFF AT 88 PERCENT TORQUE. AUTOFEATHER WOULD NOT ARM. RETURNED TO GATE. R & R THE RT TORQUE CONDITIONING CIRCUIT BREAKERS. RAN ENGINES IAW MANUAL CH
- [SDR HNAA2017091800311](https://openairdocs.org/sdr/HNAA2017091800311), Sep 14, 2017: WIRE HARNESS. MALFUNCTIONED. ABORTED TAKEOFF DUE TO AUTOFEATHER WOULD NOT ARM. COMPLIED WITH FLIGHT CREW PROCEDURES. REMOVED AND RANG OUT THE NR 2 ENGINE STRUT HARNESS AND REINSTALLED . CHE
- [SDR HNAA2017091400308](https://openairdocs.org/sdr/HNAA2017091400308), Sep 13, 2017: AUTOFEATHER SYS. MALFUNCTIONED. AUTO FEATHER FAILED TO ARM AT 65 KTS. REJECTED T/O AND RETURNED TO THE GATE. R & R THE NR 1 ENGINE, COMPLIED WITH AUTO FEATHER AND AUX FEATHER RUNS, IAW SRT MAN
- [SDR HNAA2017091400303](https://openairdocs.org/sdr/HNAA2017091400303), Sep 8, 2017: ACTUATOR. FAILED. AUTO FX WOULD NOT ARM. ABORTED TAKE OFF. R & R ACTUATORS FOR 6121-S10,11 FOR BEING FLAT SPOTTED. R & R CIRCUIT BREAKERS FOR LT G-10 & RT G10. CHECKED AUTO FX PO
- [SDR HNAA2017082800295](https://openairdocs.org/sdr/HNAA2017082800295), Aug 26, 2017: AUTOFEATHER SYS. MALFUNCTIONED. AUTOFEATHER WOULD NOT ARM AT 90 PERCENT TQ. ABORTED TAKEOFF.
- [SDR HNAA2017082800294](https://openairdocs.org/sdr/HNAA2017082800294), Aug 26, 2017: POTENTIOMETER. OUT OF RIG. REJECTED TAKE-OFF DUE TO A/F ARM LIGHT NOT ON 90 PERCENT TQ. FACT: CHECK AUTO-FEATHER ARMING POTENTIOMETER USING B.O.B AND FOUND TO BE OUT OF RIGGED. RE-RIGGED 
- [SDR HNAA2017082500286](https://openairdocs.org/sdr/HNAA2017082500286), Aug 24, 2017: AUTOFEATHER SYS. MALFUNCTIONED. REJECTED TAKEOFF DUE TO AUTOFEATHER NOT ARMING UP TO 90% TORQUE. R & R THE NR 1 TSEU. GROUND RAN ACFT. AUTO-FEATHER SYSTEM OPS NORMAL IAW RUNUP MANUAL,. OK FOR 
- [SDR HNAA2017082400464](https://openairdocs.org/sdr/HNAA2017082400464), Aug 24, 2017: AUTOFEATHER SYS. MALFUNCTIONED. TAKEOFF REJECTED WITH TORQUE SET AT APPROX. 85 PERCENT DUE TO AUTO FEATHER NOT ARMING. RAN AIRCRAFT AND CHECKED OPERATION OF AUTO FEATHER IAW MANUAL AND AUTO FE
- [SDR HNAA2017082400463](https://openairdocs.org/sdr/HNAA2017082400463), Aug 24, 2017: AUTOFEATHER SYS. MALFUNCTIONED. TAKEOFF REJECTED WITH TORQUE SET AT APPROXIMATELY 85 PERCENT DUE TO AUTO FEATHER NOT ARMING. RAN AIRCRAFT AND CHECKED OPERATION OF AUTO FEATHER IAW MANUAL AND A
- [SDR HNAA2017082400462](https://openairdocs.org/sdr/HNAA2017082400462), Aug 24, 2017: SWITCH. DIRTY. AUTO FEATHER FAILS TO ARM, RETURNED TO GATE. CLEANED THE SWITCHES 6121S6-611. OPS CHECKED GOOD.
- [SDR HNAA2017080700263](https://openairdocs.org/sdr/HNAA2017080700263), Aug 6, 2017: CONTROL UNIT. MALFUNCTIONED. AUTOFEATHER FAILED TO ARM AT 86% TQ, REJECTED TAKE OFF. R & R THE NR 2 ENG TSCU AND RELAY 6121K5 IAW 72-01-10 AND OPS CHECKED GOOD.
- [SDR HNAA2017070700228](https://openairdocs.org/sdr/HNAA2017070700228), Jul 5, 2017: PUMP. MALFUNCTIONED. NR 1 STANBY PUMP WILL NOT COME ON. RESET THE CIRCUIT BREAKER. OPS NORMAL. NO DEFECTS. OK FOR SERVICE.
- [SDR HNAA2017061400205](https://openairdocs.org/sdr/HNAA2017061400205), Jun 11, 2017: WARNING MESSAGE. FALSE ACTIVATION. DURING TAKEOFF ROLL, MASTER WARNING LIGHT ILLUMINATED INDICATING SERVICE DOOR WAS NOT CLOSED. INSPECTED THE SERVICE DOOR, NO DEFECTS NOTED. OK FOR SERVICE
- [SDR HNAA2017040500105](https://openairdocs.org/sdr/HNAA2017040500105), Apr 3, 2017: RADAR. FAILED. RADAR FAILED IN FLIGHT. R & R RADAR RIGHT. OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR HNAA2017032000090](https://openairdocs.org/sdr/HNAA2017032000090), Mar 19, 2017: WARNING LIGHT. FALSE ACTIVATION. DURING GEAR RETRACTION GEAR DID NOT RETRACT. THREE AMBER AND RED LIGHTS ON BOTH MAINS. PERFORMED ALTERNATE EXTENSION GEAR DOWN AND LOCKED. SWUNG GEAR MULTIPLE T
- [SDR HNAA2016120900350](https://openairdocs.org/sdr/HNAA2016120900350), Dec 9, 2016: PANEL. MALFUNCTIONED. 1 AND 2 ENGINES HAD 15 PERCENT TORQUE SURGES AT 400 FEET ALTITUDE. REACHED 105 PERCENT TORQUE. REDUCED TORQUE TO 4 PERCENT. SURGE STOPPED. RETURNED TO FIELD. RE
- [SDR HNAA2016121200386](https://openairdocs.org/sdr/HNAA2016121200386), Dec 8, 2016: PANEL. MALFUNCTIONED. NR 1 AND 2 ENGINES HAD 15 PERCENT TORQUE SURGES AT 400 FT.ALTITUDE. REACHED 105 PERCENT TORQUE. REDUCED TORQUE TO 45 PERCENT. SURGING STOPPED. RETURNED TO FIELD
- [SDR HNAA2016120500376](https://openairdocs.org/sdr/HNAA2016120500376), Dec 5, 2016: APU. FAILED. APU FAILED AFTER 20 MINUTES RUNNING TIME WITH BLEEDS OPEN AND CABIN PACK RUNNING.TRIGGERED CHECK FIRE DETECT WARNING LIGHT. AFTER SHUTDOWN. INSPECTED APU COMPAR
- [SDR HNAA2016120500372](https://openairdocs.org/sdr/HNAA2016120500372), Dec 5, 2016: BULB. INOPERATIVE. EMERGENCY LIGHT IS INOPERATIVE AT ROW 1. REMOVED AND REPLACED THE BULBS. OPS CHECKED GOOD.
- [SDR HNAA2016112100353](https://openairdocs.org/sdr/HNAA2016112100353), Nov 21, 2016: BULB. INOPERATIVE. DIM EMERGENCY LIGHT ON RIGHT AFT SIDE OF FUSELAGE. REMOVED AND REPLACED THE BULB. OPS CHECKED GOOD.
- [SDR HNAA2016112100352](https://openairdocs.org/sdr/HNAA2016112100352), Nov 21, 2016: BATTERY PACK. INOPERATIVE. EMERGENCY LIGHTS AT RIGHT AFT SIDE OF FUSELAGE, CENTER AISLE EXIT SIGN AT ROW 11, AND CENTER OVERHEAD LIGHTS AT ROW 9 AND 13 ARE INOPERATIVE. REMOVED AND REPLAC
- [SDR HNAA2016101900321](https://openairdocs.org/sdr/HNAA2016101900321), Oct 19, 2016: APU. ODOR. BURNED OIL ODOR IN CABIN AND FLIGHT DECK WHEN USING APU BLEEDS. GROUND RAN AIRCRAFT AND CONFIRMED OIL IN APU BLEEDS. GOES AWAY WITH ENGINE BLEEDS.
- [SDR HNAA2016093000302](https://openairdocs.org/sdr/HNAA2016093000302), Sep 30, 2016: LIGHT. INOPERATIVE. FIRST EMERGENCY FLOOR LIGHT FROM FRONT IS INOP. REMOVED AND REPLACED BULB. OPS CHECKED GOOD.
- [SDR HNAA2016061700183](https://openairdocs.org/sdr/HNAA2016061700183), Jun 16, 2016: HYDRAULIC LINE. LEAKING. NR 2 HYD QTY WENT TO ZERO AFTER STARTUP. NR 2 NACELLE WET AROUND BRAKES. BOTH ENGINES SHUTDOWN IN LESS THAN A MINUTE. NR 2 HYD QTY IN NACELLE APPEARS TO BE ZERO
- [SDR HNAA2016061700184](https://openairdocs.org/sdr/HNAA2016061700184), Jun 16, 2016: MONITOR. DEFECTIVE. WHEN APU SHUTS DOWN A NEGATIVE LOAD DISPLAYED. NO, HAD TO RETURN TO GATE, CX'D AFTER HEA. RING SUSPECTED CONTACTOR WELDED, LATE ACFT. VERIFIED APU GEN CONTACTOR
- [SDR HNAA2016050400130](https://openairdocs.org/sdr/HNAA2016050400130), May 2, 2016: LIGHT. DIM. LEFT AFT EMERGENCY EXIT DOOR LIGHT DIM. R & R LIGHT .
- [SDR HNAA2016050400129](https://openairdocs.org/sdr/HNAA2016050400129), May 2, 2016: BULB. INOPERATIVE. 7DF FLOOR EMERGENCY LIGHT INOPERATIVE. R & R BULB, OPS CHECK GOOD.
- [SDR HNAA2016021200033](https://openairdocs.org/sdr/HNAA2016021200033), Feb 9, 2016: UNKNOWN. ODOR. BURNING ODOR IN CABIN AFTER APPLYING POWER TO ACFT. NO, MELD APU BLEED, RAN APU WITH AND WITHOUT BLEEDS ON. INSPECTED APU BLEED DUCTS AND ACM AND HEAT EXCHANGER
- [SDR HNAA2015071300225](https://openairdocs.org/sdr/HNAA2015071300225), Jul 13, 2015: BATTERY PACK. INOPERATIVE. AFT FUSELAGE EMERGENCY LIGHT IS INOPERATIVE ON RT SIDE. R & R EMERGENCY LIGHT BATTERIES IAW WORD CARD 33-50-05R.
- [SDR HNAA2015071300224](https://openairdocs.org/sdr/HNAA2015071300224), Jul 13, 2015: POWER SUPPLY. INOPERATIVE. FORWARD LT EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. R & R PS1 EMERGENCY LIGHT BASE POWER SUPPLY IAW MM 33-51-05.
- [SDR HNAA2015062400204](https://openairdocs.org/sdr/HNAA2015062400204), Jun 24, 2015: SEQUENCE VALVE. MALFUNCTIONED. LEVELING OFF A 10,000 FEE, NLG AMBER DOOR LIGHT ILLUMINATED ALONG WITH UNSAFE INDICATION AND NOISE FROM NLG AREA. INDICATION CLEARED AND REMAINED NORMAL FOR RES
- [SDR HNAA2015051900163](https://openairdocs.org/sdr/HNAA2015051900163), May 16, 2015: AUDIO PANEL. FAILED. ODOR AND SMOKE IN FLIGHT IN FRONT PART OF CABIN. EMERGENCY CALL LIGHT FLICKERED AND WAS STUCK. INSPECTED AND FOUND FWD. F/A INTERPHONE CONTROL PANEL WITH FAILED
- [SDR HNAA2015031600100](https://openairdocs.org/sdr/HNAA2015031600100), Mar 16, 2015: BULB. INOPERATIVE. 4TH FLOOR PATH EMERGENCY LIGHT IS INOPERATIVE. R & R BULB AT FLOOR EMERGENCY PATH LIGHT. OPS CHECKED GOOD.
- [SDR HNAA2015021300044](https://openairdocs.org/sdr/HNAA2015021300044), Feb 13, 2015: LIGHT. BROKEN. UPPER EMERGENCY F/A SIDEWALL IS BROKEN. REMOVED SHIELD, REPLACED EMERGENCY LIGHT AND REINSTALLED HARDWARE AS REQUIRED. OPS CHECKED GOOD.
- [SDR HNAA2014122400381](https://openairdocs.org/sdr/HNAA2014122400381), Dec 24, 2014: LIGHT. MALFUNCTIONED. FLOOR EMERGENCY LIGHTS WILL NOT CYCLE OFF, AFTER ACFT POWERED DOWN. STARTED APU, CYCLED EMERGENCY LIGHT SWITCH ON AND OFF. LIGHTS WENT OFF. OPERATING NORMAL AT 
- [SDR HNAA2014121500364](https://openairdocs.org/sdr/HNAA2014121500364), Dec 15, 2014: CDU. FAILED. UNS SCREEN WENT BLANK ASSOCIATED WITH ELECTRICAL ODOR. R & R UNS1C CDU IAW MM 34-61-30. UNS SYS OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR HNAA2014111700325](https://openairdocs.org/sdr/HNAA2014111700325), Nov 17, 2014: POWER SUPPLY. MALFUNCTIONED. EMERGENCY LIGHT ABOVE UNDER WING EXIT TURNED ON IN FLIGHT. TURNED OFF 3 MINUTES PRIOR TO LANDING. R & R LIGHT POWER SUPPLY AND BATTERY AT 3351-PS3 IAW 33-51-05.
- [SDR HNAA2014082000245](https://openairdocs.org/sdr/HNAA2014082000245), Aug 20, 2014: BULB. INOPERATIVE. EMERGENCY CEILING LIGHT IS INOPERATIVE AT ROW 9. R & R BULB, OPS CHECKED GOOD.
- [SDR HNAA2014082000243](https://openairdocs.org/sdr/HNAA2014082000243), Aug 20, 2014: TRANSCEIVER. INOPERATIVE. WEATHER RADAR DOES NOT PAINT KNOWN WEATHER. R & R RADAR RT. OPS CHECKED GOOD.
- [SDR HNAA2014081100229](https://openairdocs.org/sdr/HNAA2014081100229), Aug 11, 2014: BULB. INOPERATIVE. VARIOUS EMERGENCY LIGHTS ARE OUT ON EXIT SIGNS. R & R BULB. OPS CHECKED GOOD.
- [SDR HNAA2014041800133](https://openairdocs.org/sdr/HNAA2014041800133), Apr 18, 2014: BULB. INOPERATIVE. EMERGENCY LIGHT CENTER CEILING IS INOPERATIVE IN ROW 10. R & R BULB0. OPS CHECKED GOOD.
- [SDR HNAA2014030700078](https://openairdocs.org/sdr/HNAA2014030700078), Mar 6, 2014: SMOKE DETECTOR. MALFUNCTIONED. SMOKE DETECTOR LIGHT CAME ON AND REMAINS ILLUMINATED. CREW CHECKED CARGO BAY AND NO SMOKE FOUND. WHILE TAKING RIGHT UP FROM THE CREW - THE LIGHT EXTINGUISHED ON
- [SDR HNAA2014021200041](https://openairdocs.org/sdr/HNAA2014021200041), Feb 12, 2014: BULB. FAILED. OVERHEAD EMERGENCY CEILING LIGHT IS INOPERATIVE AT ROW 10. REMOVED LENS, R & R BULB. REINSTALLED LENS. OPS CHECKED GOOD.
- [SDR HNAA2013120900613](https://openairdocs.org/sdr/HNAA2013120900613), Dec 9, 2013: AHRS. MALFUNCTIONED. DURING TAXI OUT, NR 2 AHRS DISPLAYED PITCH AND ROLL MISMATCH WITH AHRS DATA INVALID ON 802 PANEL. ADI ROLLED 60 DEGREES AND PITCHED 60 DEGREES UP AND DOWN. R & 

All 152: https://openairdocs.org/deregistered/N336EN-2020-03-20/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20070118001419I](https://openairdocs.org/incident/20070118001419I), Jan 18, 2007: Dhav DHC8311 (N336EN), Charlottesville, VA, Minor damage. (-23) 01/18/2007, At 1137E, piedmont airlines flight 4339, a DHC-8-311, diverted to cho and landed on runway 21 after reporting an electrical fire in the…

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